Blade for a turbine engine and method for production of said...

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – Specific casing or vane material

Reexamination Certificate

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C415S208100, C415S211200, C416S232000, C416S24100B, C029S463000, C029S889720, C029S889721, C228S165000, C228S171000, C228S193000

Reexamination Certificate

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07438523

ABSTRACT:
A blade for a turbine engine is described, having a base body, made from a titanium alloy, with a first and a second component piece, which are connected in the connection region by means of a bonding process. A groove with a groove wall runs through the connection region, to prevent local concentration of tension, such that the above borders directly on the second component piece and forms therewith a connection angle greater than 70 degrees.

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